EP2562352A3 - Appareil de traitement d'un ensemble d'aubes et procédé de traitement d'ensemble d'aubes - Google Patents
Appareil de traitement d'un ensemble d'aubes et procédé de traitement d'ensemble d'aubes Download PDFInfo
- Publication number
- EP2562352A3 EP2562352A3 EP12180003.1A EP12180003A EP2562352A3 EP 2562352 A3 EP2562352 A3 EP 2562352A3 EP 12180003 A EP12180003 A EP 12180003A EP 2562352 A3 EP2562352 A3 EP 2562352A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- bucket assembly
- platform
- cooling circuit
- airfoil
- treating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title abstract 2
- 238000001816 cooling Methods 0.000 abstract 9
- 239000012530 fluid Substances 0.000 abstract 2
- 239000002826 coolant Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/186—Film cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Heat Treatments In General, Especially Conveying And Cooling (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/214,583 US9447691B2 (en) | 2011-08-22 | 2011-08-22 | Bucket assembly treating apparatus and method for treating bucket assembly |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2562352A2 EP2562352A2 (fr) | 2013-02-27 |
EP2562352A3 true EP2562352A3 (fr) | 2018-02-21 |
EP2562352B1 EP2562352B1 (fr) | 2021-09-29 |
Family
ID=46829635
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12180003.1A Active EP2562352B1 (fr) | 2011-08-22 | 2012-08-10 | Ensemble d'aube de turbine à gaz avec refroidissement de plateforme amélioré et procédé de traitement d'un tel ensemble |
Country Status (3)
Country | Link |
---|---|
US (1) | US9447691B2 (fr) |
EP (1) | EP2562352B1 (fr) |
CN (1) | CN102953765B (fr) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9022735B2 (en) * | 2011-11-08 | 2015-05-05 | General Electric Company | Turbomachine component and method of connecting cooling circuits of a turbomachine component |
US11047241B2 (en) * | 2013-09-19 | 2021-06-29 | Raytheon Technologies Corporation | Gas turbine engine airfoil having serpentine fed platform cooling passage |
US10001018B2 (en) | 2013-10-25 | 2018-06-19 | General Electric Company | Hot gas path component with impingement and pedestal cooling |
JP6613803B2 (ja) | 2015-10-22 | 2019-12-04 | 三菱日立パワーシステムズ株式会社 | 翼、これを備えているガスタービン、及び翼の製造方法 |
US20180230815A1 (en) * | 2017-02-15 | 2018-08-16 | Florida Turbine Technologies, Inc. | Turbine airfoil with thin trailing edge cooling circuit |
US10508548B2 (en) * | 2017-04-07 | 2019-12-17 | General Electric Company | Turbine engine with a platform cooling circuit |
US11506061B2 (en) * | 2020-08-14 | 2022-11-22 | Mechanical Dynamics & Analysis Llc | Ram air turbine blade platform cooling |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4134709A (en) * | 1976-08-23 | 1979-01-16 | General Electric Company | Thermosyphon liquid cooled turbine bucket |
JPH0211801A (ja) * | 1988-06-29 | 1990-01-16 | Hitachi Ltd | ガスタービン冷却動翼 |
EP0937863A2 (fr) * | 1998-02-23 | 1999-08-25 | Mitsubishi Heavy Industries, Ltd. | Plateforme pour une aube mobile d'une turbine à gaz |
US20060056970A1 (en) * | 2004-09-15 | 2006-03-16 | General Electric Company | Apparatus and methods for cooling turbine bucket platforms |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3066910A (en) * | 1958-07-09 | 1962-12-04 | Thompson Ramo Wooldridge Inc | Cooled turbine blade |
DE1801475B2 (de) * | 1968-10-05 | 1971-08-12 | Daimler Benz Ag, 7000 Stuttgart | Luftgekuehlte turbinenschaufel |
US4312625A (en) * | 1969-06-11 | 1982-01-26 | The United States Of America As Represented By The Secretary Of The Air Force | Hydrogen cooled turbine |
US4244676A (en) * | 1979-06-01 | 1981-01-13 | General Electric Company | Cooling system for a gas turbine using a cylindrical insert having V-shaped notch weirs |
US4350473A (en) * | 1980-02-22 | 1982-09-21 | General Electric Company | Liquid cooled counter flow turbine bucket |
US5382135A (en) * | 1992-11-24 | 1995-01-17 | United Technologies Corporation | Rotor blade with cooled integral platform |
US5536143A (en) * | 1995-03-31 | 1996-07-16 | General Electric Co. | Closed circuit steam cooled bucket |
US5848876A (en) * | 1997-02-11 | 1998-12-15 | Mitsubishi Heavy Industries, Ltd. | Cooling system for cooling platform of gas turbine moving blade |
JP3758792B2 (ja) * | 1997-02-25 | 2006-03-22 | 三菱重工業株式会社 | ガスタービン動翼のプラットフォーム冷却機構 |
JP3411775B2 (ja) * | 1997-03-10 | 2003-06-03 | 三菱重工業株式会社 | ガスタービン動翼 |
JP3457831B2 (ja) * | 1997-03-17 | 2003-10-20 | 三菱重工業株式会社 | ガスタービン動翼の冷却プラットフォーム |
US6092983A (en) * | 1997-05-01 | 2000-07-25 | Mitsubishi Heavy Industries, Ltd. | Gas turbine cooling stationary blade |
US5915923A (en) * | 1997-05-22 | 1999-06-29 | Mitsubishi Heavy Industries, Ltd. | Gas turbine moving blade |
CA2231988C (fr) * | 1998-03-12 | 2002-05-28 | Mitsubishi Heavy Industries, Ltd. | Pale de turbine a gaz |
US6390774B1 (en) * | 2000-02-02 | 2002-05-21 | General Electric Company | Gas turbine bucket cooling circuit and related process |
US6402471B1 (en) * | 2000-11-03 | 2002-06-11 | General Electric Company | Turbine blade for gas turbine engine and method of cooling same |
US6481972B2 (en) * | 2000-12-22 | 2002-11-19 | General Electric Company | Turbine bucket natural frequency tuning rib |
JP3776897B2 (ja) | 2003-07-31 | 2006-05-17 | 三菱重工業株式会社 | ガスタービン動翼のプラットフォーム冷却機構 |
US7255536B2 (en) * | 2005-05-23 | 2007-08-14 | United Technologies Corporation | Turbine airfoil platform cooling circuit |
US7309212B2 (en) * | 2005-11-21 | 2007-12-18 | General Electric Company | Gas turbine bucket with cooled platform leading edge and method of cooling platform leading edge |
US7513738B2 (en) * | 2006-02-15 | 2009-04-07 | General Electric Company | Methods and apparatus for cooling gas turbine rotor blades |
US7416391B2 (en) | 2006-02-24 | 2008-08-26 | General Electric Company | Bucket platform cooling circuit and method |
US7553131B2 (en) * | 2006-07-21 | 2009-06-30 | United Technologies Corporation | Integrated platform, tip, and main body microcircuits for turbine blades |
US7819629B2 (en) * | 2007-02-15 | 2010-10-26 | Siemens Energy, Inc. | Blade for a gas turbine |
JP5281245B2 (ja) | 2007-02-21 | 2013-09-04 | 三菱重工業株式会社 | ガスタービン動翼のプラットフォーム冷却構造 |
US7845907B2 (en) * | 2007-07-23 | 2010-12-07 | United Technologies Corporation | Blade cooling passage for a turbine engine |
US8096772B2 (en) * | 2009-03-20 | 2012-01-17 | Siemens Energy, Inc. | Turbine vane for a gas turbine engine having serpentine cooling channels within the inner endwall |
-
2011
- 2011-08-22 US US13/214,583 patent/US9447691B2/en active Active
-
2012
- 2012-08-10 EP EP12180003.1A patent/EP2562352B1/fr active Active
- 2012-08-22 CN CN201210299794.7A patent/CN102953765B/zh active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4134709A (en) * | 1976-08-23 | 1979-01-16 | General Electric Company | Thermosyphon liquid cooled turbine bucket |
JPH0211801A (ja) * | 1988-06-29 | 1990-01-16 | Hitachi Ltd | ガスタービン冷却動翼 |
EP0937863A2 (fr) * | 1998-02-23 | 1999-08-25 | Mitsubishi Heavy Industries, Ltd. | Plateforme pour une aube mobile d'une turbine à gaz |
US20060056970A1 (en) * | 2004-09-15 | 2006-03-16 | General Electric Company | Apparatus and methods for cooling turbine bucket platforms |
Also Published As
Publication number | Publication date |
---|---|
EP2562352B1 (fr) | 2021-09-29 |
US9447691B2 (en) | 2016-09-20 |
CN102953765B (zh) | 2016-04-27 |
CN102953765A (zh) | 2013-03-06 |
US20130052009A1 (en) | 2013-02-28 |
EP2562352A2 (fr) | 2013-02-27 |
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